JP2023071646A5 - - Google Patents
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- JP2023071646A5 JP2023071646A5 JP2023007018A JP2023007018A JP2023071646A5 JP 2023071646 A5 JP2023071646 A5 JP 2023071646A5 JP 2023007018 A JP2023007018 A JP 2023007018A JP 2023007018 A JP2023007018 A JP 2023007018A JP 2023071646 A5 JP2023071646 A5 JP 2023071646A5
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- Prior art keywords
- aerial vehicle
- support line
- mothership
- length
- vehicle
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Claims (19)
母船であって、前記母船は、前記母船が非ダクトローターを介して推力を生成することによって垂直離着陸を可能にするような回転翼航空機である、母船と、
空中車両であって、前記空中車両は、前記空中車両が非ダクトローターを介して推力を生成するような回転翼航空機である、空中車両と、
前記母船と前記空中車両の間に配設されるウインチシステムであって、前記ウインチシステムは、支持線を有し、かつ、前記支持線の長さを調整するように作動するように構成されている、ウインチシステムと、
前記空中車両への風の状態を検出し、風への応答を判定するように構成されたコントローラと、を備え、
風への応答を判定することは、
前記空中車両の前記ローターの揚力の大きさを調整することであって、前記空中車両の前記ローターの揚力の大きさを調整することは、前記空中車両の前記ローターに、前記風の状態によって生成される力を少なくとも部分的に打ち消すために非垂直推力を生成するように指示することを含む、前記空中車両の前記ローターの揚力の大きさを調整することと、
前記支持線の前記長さを調整することであって、前記支持線の前記長さを調整することは、前記ウインチシステムに、前記支持線内の張力を協調させるために前記支持線を巻き付けることによって前記空中車両の垂直加重の少なくとも一部を担うように指示することを含む、前記支持線の前記長さを調整すること、の一方または両方を含む、
空中車両システム。 An aerial vehicle system,
a mothership, said mothership being a rotary wing aircraft such that said mothership is capable of vertical take-off and landing by generating thrust through non-ducted rotors;
an airborne vehicle, said airborne vehicle being a rotorcraft such that said airborne vehicle generates thrust through non-ducted rotors;
A winch system disposed between the mothership and the aerial vehicle, the winch system having a support line and configured to operate to adjust the length of the support line. with a winch system,
a controller configured to detect wind conditions to the aerial vehicle and determine a response to the wind ;
Determining the response to wind is
adjusting the magnitude of the lift force of the rotor of the aerial vehicle, wherein adjusting the magnitude of the lift force of the rotor of the aerial vehicle generates on the rotor of the aerial vehicle according to the wind conditions; adjusting the magnitude of the lift force of the rotor of the airborne vehicle, including directing it to generate a non-vertical thrust to at least partially counteract the applied force;
adjusting the length of the support line, wherein adjusting the length of the support line winds the winch system around the support line to coordinate tension in the support line. adjusting the length of the support line, including directing it to bear at least a portion of the vertical weight of the aerial vehicle by
aerial vehicle system.
空中車両への風の状態に関する情報を受け取ることであって、前記空中車両は、前記空中車両が推力を生成する回転翼航空機である、情報を受け取ること、 receiving information about wind conditions to an airborne vehicle, said airborne vehicle being a rotorcraft in which said airborne vehicle produces thrust;
前記空中車両の風への応答を判定すること、 determining a response of the aerial vehicle to wind;
支持線に対する前記空中車両の垂直荷重の少なくとも一部を担うために、前記空中車両に取り付けられた前記支持線の長さに対して行われる必要のある調整を判定すること、 determining adjustments that need to be made to the length of the support line attached to the aerial vehicle to carry at least a portion of the vertical load of the aerial vehicle relative to the support line;
非垂直推力を生成するために前記空中車両のスラスターに対して行われる必要のある調整を判定すること、かつ、 determining adjustments that need to be made to the airborne vehicle's thrusters to produce non-vertical thrust; and
前記空中車両の位置に対する前記風の状態の影響の少なくとも一部を打ち消すために、前記支持線、または、前記スラスターを制御すること、 controlling the support line or the thrusters to at least partially counteract the effects of the wind conditions on the position of the aerial vehicle;
を行うように構成されたコントローラを備える、空中車両システムを制御するシステム。 A system for controlling an aerial vehicle system, comprising a controller configured to:
空中車両への風の状態に関する情報を受け取ることであって、前記空中車両は、前記空中車両が推力を生成する回転翼航空機である、情報を受け取ること、
前記空中車両の風への応答を判定すること、
支持線に対する前記空中車両の垂直荷重の少なくとも一部を担うために、前記空中車両に取り付けられた前記支持線の長さに対して行われる必要のある調整を判定すること、
非垂直推力を生成するために前記空中車両のスラスターに対して行われる必要のある調整を判定すること、かつ、
前記空中車両の位置に対する前記風の状態の影響の少なくとも一部を打ち消すために、前記支持線、または、前記スラスターを制御すること、
を含む、空中車両システムを制御する方法。 A method of controlling an aerial vehicle system, comprising:
receiving information about wind conditions to an airborne vehicle, said airborne vehicle being a rotorcraft in which said airborne vehicle produces thrust;
determining a response of the aerial vehicle to wind;
determining adjustments that need to be made to the length of the support line attached to the aerial vehicle to carry at least a portion of the vertical load of the aerial vehicle relative to the support line;
determining adjustments that need to be made to the airborne vehicle's thrusters to produce non-vertical thrust; and
controlling the support line or the thrusters to at least partially counteract the effects of the wind conditions on the position of the aerial vehicle;
A method of controlling an aerial vehicle system, comprising :
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201962858330P | 2019-06-07 | 2019-06-07 | |
US62/858,330 | 2019-06-07 | ||
PCT/US2020/036492 WO2020247870A1 (en) | 2019-06-07 | 2020-06-05 | Suspended aerial vehicle system with thruster stabilization |
JP2021572546A JP7216845B2 (en) | 2019-06-07 | 2020-06-05 | Suspended aerial vehicle system with thruster stabilization |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2021572546A Division JP7216845B2 (en) | 2019-06-07 | 2020-06-05 | Suspended aerial vehicle system with thruster stabilization |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2023071646A JP2023071646A (en) | 2023-05-23 |
JP2023071646A5 true JP2023071646A5 (en) | 2023-06-23 |
Family
ID=73652308
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2021572546A Active JP7216845B2 (en) | 2019-06-07 | 2020-06-05 | Suspended aerial vehicle system with thruster stabilization |
JP2023007018A Pending JP2023071646A (en) | 2019-06-07 | 2023-01-20 | Suspended aerial vehicle system with thruster stabilization |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2021572546A Active JP7216845B2 (en) | 2019-06-07 | 2020-06-05 | Suspended aerial vehicle system with thruster stabilization |
Country Status (12)
Country | Link |
---|---|
US (3) | US11319065B2 (en) |
EP (1) | EP3980330A4 (en) |
JP (2) | JP7216845B2 (en) |
KR (2) | KR102548185B1 (en) |
CN (1) | CN114144353A (en) |
AU (2) | AU2020287661B2 (en) |
BR (1) | BR112021024619B1 (en) |
CA (1) | CA3142927A1 (en) |
IL (2) | IL288688B (en) |
MX (1) | MX2021015023A (en) |
NZ (1) | NZ783718A (en) |
WO (1) | WO2020247870A1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2020250484A1 (en) * | 2019-06-14 | 2020-12-17 | パナソニック インテレクチュアル プロパティ コーポレーション オブ アメリカ | Elevating system |
CN113093809A (en) * | 2021-04-12 | 2021-07-09 | 北京理工大学 | Active disturbance rejection controller of composite wing unmanned aerial vehicle and establishing method thereof |
US11939054B2 (en) * | 2022-06-16 | 2024-03-26 | HazelAero | Vertical takeoff and landing aircraft surface tension compensation system |
KR102692624B1 (en) * | 2022-10-19 | 2024-08-06 | 주식회사 승인디에프에스 | Auxiliary drone for lifting steel structures |
CN118004432B (en) * | 2024-04-08 | 2024-06-11 | 北京中航智科技有限公司 | Engine pitch-and-depression adjusting suspension structure, aircraft power system and aircraft |
Family Cites Families (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4267987A (en) * | 1979-03-29 | 1981-05-19 | Mcdonnell William R | Helicopter airborne load systems and composite aircraft configurations |
US6913224B2 (en) * | 2003-09-29 | 2005-07-05 | Dana R. Johansen | Method and system for accelerating an object |
US8157205B2 (en) | 2006-03-04 | 2012-04-17 | Mcwhirk Bruce Kimberly | Multibody aircrane |
US20110192938A1 (en) * | 2010-02-09 | 2011-08-11 | Northrop Grumman Systems Corporation | Wind power generation system for lighter than air (lta) platforms |
US9623949B2 (en) * | 2011-03-15 | 2017-04-18 | Stratospheric Airships, Llc | Systems and methods for long endurance airship operations |
IL217070A0 (en) * | 2011-12-18 | 2012-03-29 | Ofek Eshkolot Res And Dev Ltd | Aircraft with fixed and tilting thrusters |
DE102012002067A1 (en) * | 2012-02-03 | 2013-08-08 | Eads Deutschland Gmbh | Air-to-ground monitoring and / or control system and method for airborne inspection and / or control of offshore or offshore objects |
SG194257A1 (en) * | 2012-04-26 | 2013-11-29 | Yik Hei Sia | Power generating windbags and water-bags |
US10144511B2 (en) | 2013-04-02 | 2018-12-04 | Hood Technology Corporation | Helicopter-mediated system and method for launching and retrieving an aircraft |
US9346547B2 (en) * | 2013-08-26 | 2016-05-24 | Google Inc. | Mechanisms for lowering a payload to the ground from a UAV |
US9205921B1 (en) * | 2013-12-19 | 2015-12-08 | Google Inc. | Methods and systems for conserving power during hover flight |
US9849981B1 (en) * | 2014-08-28 | 2017-12-26 | X Development Llc | Payload-release device position tracking |
US11341610B2 (en) * | 2014-11-13 | 2022-05-24 | The Boeing Company | Deployable airborne sensor array system and method of use |
US9630712B1 (en) * | 2015-09-23 | 2017-04-25 | Amazon Technologies, Inc. | Using multirotor lifters to deploy fixed wing aircraft |
US10933997B2 (en) * | 2015-10-02 | 2021-03-02 | Insitu, Inc. | Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods |
IL242418B (en) * | 2015-11-03 | 2020-05-31 | Israel Aerospace Ind Ltd | Hovering aerial vehicle and method of flyins same |
US11325702B2 (en) * | 2016-08-19 | 2022-05-10 | Motorola Solutions, Inc. | Tethered aerial drone system |
US11505330B2 (en) * | 2016-08-20 | 2022-11-22 | Modern Technology Solutions, Inc. | Refueling system and systems with end effectors |
JP2018134242A (en) * | 2017-02-22 | 2018-08-30 | 公立大学法人大阪市立大学 | Fire fighting system, fire fighting method, control device, and control method |
US20180297699A1 (en) * | 2017-04-18 | 2018-10-18 | Mesa Digital, Llc | Overhead tethered drone system |
CN109923488A (en) * | 2017-04-27 | 2019-06-21 | 深圳市大疆创新科技有限公司 | The system and method for generating real-time map using loose impediment |
US10745107B1 (en) * | 2017-05-08 | 2020-08-18 | Government Of The United States, As Represented By The Secretary Of The Air Force | Rapid flap deflection for high lift transients |
CN107792371B (en) * | 2017-09-27 | 2020-10-13 | 北京航空航天大学 | Aerial towline towing target system-based unmanned aerial vehicle air-based rapid launching device and method |
JP2019085104A (en) | 2017-11-06 | 2019-06-06 | 株式会社エアロネクスト | Flight unit and control method of flight unit |
US10479503B2 (en) * | 2018-02-08 | 2019-11-19 | Vita Inclinata Technologies, Inc. | Suspended load stability systems and methods |
US10919624B2 (en) * | 2018-08-06 | 2021-02-16 | Wet | UAS display system and method |
US10884415B2 (en) * | 2018-12-28 | 2021-01-05 | Intel Corporation | Unmanned aerial vehicle light flash synchronization |
US20210147080A1 (en) * | 2019-11-18 | 2021-05-20 | Agco Corporation | Crop-extraction system having an unmanned aerial vehicle, and related methods |
-
2020
- 2020-06-05 IL IL288688A patent/IL288688B/en unknown
- 2020-06-05 IL IL296077A patent/IL296077A/en unknown
- 2020-06-05 NZ NZ783718A patent/NZ783718A/en unknown
- 2020-06-05 JP JP2021572546A patent/JP7216845B2/en active Active
- 2020-06-05 CA CA3142927A patent/CA3142927A1/en active Pending
- 2020-06-05 KR KR1020227000629A patent/KR102548185B1/en active Application Filing
- 2020-06-05 MX MX2021015023A patent/MX2021015023A/en unknown
- 2020-06-05 EP EP20818431.7A patent/EP3980330A4/en active Pending
- 2020-06-05 BR BR112021024619-3A patent/BR112021024619B1/en active IP Right Grant
- 2020-06-05 AU AU2020287661A patent/AU2020287661B2/en active Active
- 2020-06-05 WO PCT/US2020/036492 patent/WO2020247870A1/en unknown
- 2020-06-05 KR KR1020237020977A patent/KR20230097220A/en not_active Application Discontinuation
- 2020-06-05 CN CN202080051830.0A patent/CN114144353A/en active Pending
-
2021
- 2021-01-15 US US17/151,035 patent/US11319065B2/en active Active
- 2021-12-22 US US17/645,544 patent/US11814168B2/en active Active
-
2022
- 2022-05-17 AU AU2022203308A patent/AU2022203308B2/en active Active
-
2023
- 2023-01-20 JP JP2023007018A patent/JP2023071646A/en active Pending
- 2023-11-09 US US18/505,652 patent/US20240343419A1/en active Pending
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